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Integral oil tank and manufacturing method thereof

A technology of integral fuel tank and manufacturing method, which is applied to the fuel tank of the power unit, other household appliances, household components, etc., can solve the problems of high oil leakage risk of the fuel tank, increase the difficulty of sealing, etc., and reduce the skin to seam and the structural weight of the fuel tank The effect of reducing the difficulty of sealing

Pending Publication Date: 2021-09-24
HIWING AVIATION GENERAL EQUIP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

The sealant seal overall fuel tank generally adopts a skeleton skin structure, and the skin is formed by composite materials, which effectively reduces the structural weight, but this kind of fuel tank has many standard parts for connection, the number of holes is large, and the skin has many seams , which increases the difficulty of sealing, so that there is a high risk of oil leakage during the use of the formed fuel tank

Method used

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  • Integral oil tank and manufacturing method thereof
  • Integral oil tank and manufacturing method thereof
  • Integral oil tank and manufacturing method thereof

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Embodiment Construction

[0037] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. The following description of at least one exemplary embodiment is merely illustrative in nature and in no way taken as limiting the invention, its application or uses. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0038] It should be noted that the terminology used here is only for describing specific implementations, and is not intended to limit t...

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Abstract

According to the integral oil tank and the manufacturing method thereof, the integral oil tank comprises a framework and a skin, the framework is of a main force transmission structure, the skin is made of a whole composite material, the skin and the framework are integrally formed and designed, the skin wraps the framework, the skin and the framework are co-glued and cured, and the position of a fuel oil filling port cover is arranged on the skin. The problems that in the prior art, the number of oil tank connecting standard parts is large, the number of formed holes is large, the number of skin butt joints is large, the sealing difficulty is large, and the formed oil tank has the high oil leakage risk in the using process are solved.

Description

technical field [0001] The invention belongs to the technical field of fuel tank design, and in particular relates to an integrally formed fuel tank. Background technique [0002] In modern aircraft structural design, rubber soft fuel tanks and integral fuel tanks are mostly used in fuel tanks, and the integral fuel tanks are further divided into conventional fuel tanks sealed with welded seals and sealants. The manufacturing process of the rubber soft fuel tank is cumbersome and complicated, the cost is high, and the volume utilization rate of the structural space is not high. Most of the welded fuel tanks are metal welded structures such as aluminum alloy or stainless steel, and the weight ratio is high. Therefore, more and more fuel tank structures adopt conventional integral fuel tanks sealed with sealant. The sealant seal overall fuel tank generally adopts a skeleton skin structure, and the skin is formed by composite materials, which effectively reduces the structural...

Claims

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Application Information

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IPC IPC(8): B64D37/06B29C70/34B29C70/68
CPCB64D37/06B29C70/342B29C70/683B29L2031/3076Y02T50/40
Inventor 刘伟韦楠楠杨晓亚王文强
Owner HIWING AVIATION GENERAL EQUIP